View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 20804U 26106.29851743 +.00000000 +00000-0 +31831-4 0 00001
2 20804 82.9419 213.6382 0038233 91.1989 328.0592 13.74560936 03
| Epoch (UTC): | 16 April 2026 07:09:51 |
| Eccentricity: | 0.0038233 |
| inclination: | 82.9419° |
| perigee height: | 955 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 213.6382° |
| argument of perigee: | 91.1989° |
| revolutions per day: | 13.74560936 |
| mean anomaly at epoch: | 328.0592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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